The arrangement features a centrifugal impeller that exhibits relatively high operating efficiency and high pressure capability, and can be easily constructed as a single piece. The arrangement is useful where relatively high operating efficiency and low cost construction are required, and it is particularly suited for manufacture by injection molding plastic. The impeller is characterized by: a) a hub that extends to a radius less than that of the impeller inlet, allowing one piece construction by an injection molding tool with no slides or action; b) blades that extend from a radius less than the hub radius at the base of the blades, allowing the base of the blades to connect to the hub; c) an impeller top shroud that has curvature in a plane that contains the impeller axis; and d) a cylindrical area ratio between 1.0 and 2∅ The blower assembly is characterized by a separate base plate positioned in close proximity to the base of the impeller blades. The base plate can be incorporated into a motor flange or a blower or motor housing.
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2. A centrifugal impeller mounted to rotate on an axis, the impeller comprising a plurality of blades, each having a leading edge and a trailing edge, an impeller hub, and a top shroud; the blades defining an impeller diameter, a cylindrical area ratio, a minimum chord length, a blade meanline length and a blade solidity; and the top shroud forming an inlet to the impeller having an impeller inlet radius; said impeller characterized in that:
a) it is injection molded in one piece; b) the impeller hub extends outwardly to a radius less than that of the impeller inlet radius; c) the blades extend outwardly from a radius less than the impeller hub radius; d) the top shroud has curvature in a plane that contains the impeller axis; e) the cylindrical area ratio is between 1.0 and 2.0; and f) said blade solidity is at least 2∅
1. A centrifugal impeller mounted to rotate on an axis, the impeller comprising a plurality of blades, each having a leading edge and a trailing edge, an impeller hub, and a top shroud; the blades defining an impeller diameter, a cylindrical area ratio, a minimum chord length, a blade meanline length and a blade solidity; and the top shroud forming an inlet to the impeller having an impeller inlet radius; said impeller characterized in that:
a) it is injection molded in one piece; b) the impeller hub extends outwardly to a radius less than that of the impeller inlet radius; c) the blades extend outwardly from a radius less than the impeller hub radius; d) the top shroud has curvature in a plane that contains the impeller axis; e) the cylindrical area ratio is between 1.0 and 2.0; and f) said minimum chord length is at least 15% of the impeller diameter.
3. A centrifugal impeller mounted to rotate on an axis, the impeller comprising a plurality of blades, each having a leading edge and a trailing edge, an impeller hub, and a top shroud; the blades defining an impeller diameter, a cylindrical area ratio, a minimum chord length, a blade meanline length and a blade solidity; and the top shroud forming an inlet to the impeller having an impeller inlet radius; said impeller characterized in that:
a) it is injection molded in one piece; b) the impeller hub extends outwardly to a radius less than that of the impeller inlet radius; c) the blades extend outwardly from a radius less than the impeller hub radius; d) the top shroud has curvature in a plane that contains the impeller axis; e) the cylindrical area ratio is between 1.0 and 2.0; and f) said blades make contact with the hub over less than 20% of the meanline length at the base of the blades.
31. A centrifugal blower assembly comprising a base plate and a centrifugal impeller;
A. said impeller being mounted to rotate on an axis, the impeller comprising a plurality of blades, each having a leading edge and a trailing edge, an impeller hub, and a top shroud; the blades defining an impeller diameter, a cylindrical area ratio, a minimum chord length, a blade meanline length and a blade solidity; and the top shroud forming an inlet to the impeller having an impeller inlet radius; said impeller characterized in that: 1) it is injection molded in one piece; 2) the impeller hub extends outwardly to a radius less than that of the impeller inlet radius; 3) the blades extend outwardly from a radius less than the impeller hub radius; 4) the top shroud has curvature in a plane that contains the impeller axis, and; 5) the cylindrical area ratio is between 1.0 and 2.0; and B. said base plate being characterized in that: 1) it extends outwardly to a radius greater than the impeller hub radius; 2) it is non-rotating; 3) the clearance between the base plate and the impeller blades is less than 10 percent of the impeller radius, 4) said base plate is curved in a plane that includes the fan axis said impeller top shroud and base plate together forming an airflow path from an inlet to an outlet.
28. A centrifugal blower assembly comprising a base plate and a centrifugal impeller;
A. said impeller being mounted to rotate on an axis, the impeller comprising a plurality of blades, each having a leading edge and a trailing edge, an impeller hub, and a top shroud; the blades defining an impeller diameter, a cylindrical area ratio, a minimum chord length, a blade meanline length and a blade solidity; and the top shroud forming an inlet to the impeller having an impeller inlet radius; said impeller characterized in that: 1) it is injection molded in one piece; 2) the impeller hub extends outwardly to a radius less than that of the impeller inlet radius; 3) the blades extend outwardly from a radius less than the impeller hub radius; 4) the top shroud has curvature in a plane that contains the impeller axis, and; 5) the cylindrical area ratio is between 1.0 and 2.0; and B. said base plate being characterized in that: 1) it extends outwardly to a radius greater than the impeller hub radius; 2) it is non-rotating, and; 3) the clearance between the base plate and the impeller blades is less than 10 percent of the impeller radius, said impeller top shroud and base plate together forming an airflow path from an inlet to an outlet, said assembly further comprising a motor and a motor flange, said base plate being integrated into said flange as a single monolithic part.
29. A centrifugal blower assembly comprising a base plate and a centrifugal impeller;
A. said impeller being mounted to rotate on an axis, the impeller comprising a plurality of blades, each having a leading edge and a trailing edge, an impeller hub, and a top shroud; the blades defining an impeller diameter, a cylindrical area ratio, a minimum chord length, a blade meanline length and a blade solidity; and the top shroud forming an inlet to the impeller having an impeller inlet radius; said impeller characterized in that: 1) it is injection molded in one piece; 2) the impeller hub extends outwardly to a radius less than that of the impeller inlet radius; 3) the blades extend outwardly from a radius less than the impeller hub radius; 4) the top shroud has curvature in a plane that contains the impeller axis, and; 5) the cylindrical area ratio is between 1.0 and 2.0; and B. said base plate being characterized in that: 1) it extends outwardly to a radius greater than the impeller hub radius; 2) it is non-rotating, and; 3) the clearance between the base plate and the impeller blades is less than 10 percent of the impeller radius, said impeller top shroud and base plate together forming an airflow path from an inlet to an outlet, said assembly further comprising a motor housing and further characterized in that the base plate is integrated into said motor housing as a single monolithic part.
4. The centrifugal impeller of
5. The centrifugal impeller of
6. The centrifugal impeller of
7. The centrifugal impeller of
8. The centrifugal impeller of
9. The centrifugal impeller of
10. The centrifugal impeller of
11. The centrifugal impeller of
12. A centrifugal blower assembly comprising a base plate and the impeller of
1) it extends outwardly to a radius greater than the impeller hub radius; 2) it is non-rotating, and; 3) the clearance between the base plate and the impeller blades is less than 10 percent of the impeller radius.
13. The centrifugal blower assembly of
14. The centrifugal blower assembly of
15. The centrifugal blower assembly of
16. The centrifugal blower assembly of
17. The centrifugal blower assembly of
18. The centrifugal blower assembly of
19. A method of making the centrifugal impeller of
20. A method of assembling the centrifugal blower assembly of
21. A method of assembling the centrifugal blower assembly of
22. A method of assembling the centrifugal blower assembly of
23. A method of assembling the centrifugal blower assembly of
24. A centrifugal blower assembly according to 13 which is sized and configured to be installed in an automotive climate control system.
25. A centrifugal blower assembly according to 14 which is sized and configured to be installed in an automotive climate control system.
26. A centrifugal blower assembly according to
27. A centrifugal blower assembly according to
30. The centrifugal blower assembly of
32. The centrifugal blower assembly of
33. The centrifugal blower assembly of
34. The centrifugal blower assembly of
35. The centrifugal blower assembly of
36. The centrifugal blower assembly of
37. A method of assembling the centrifugal blower assembly of
38. A method of assembling the centrifugal blower assembly of
39. A centrifugal blower assembly according to
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This application claims the benefit of provisional application U.S. Ser. No. 60/251,211, filed Dec. 4, 2000.
This invention relates to the general field of centrifugal blowers, such as those used for automotive climate control.
Centrifugal impellers generally include multiple blades that turn incoming airflow toward the radial direction as it moves from the impeller inlet to the impeller outlet. The blades generally are attached to, and rotate with, a hub, which defines the airflow path on the base of the impeller (the side opposite the inlet). For two-piece impellers, the top of the airflow path is established by a top shroud, which also is attached to the blades and rotates with the blades and the hub.
In automotive climate control applications (i.e., heating, ventilation and air conditioning) centrifugal impellers generally can be placed into two categories: a) low cost, single-piece impellers; and b) higher cost, higher efficiency two-piece impellers. The single-piece impellers, because of their lower cost, generally are used much more often than two-piece impellers. Two-piece impellers generally are used where the need for high efficiency or high pressure capability outweighs the cost disadvantage.
In automotive climate control applications, centrifugal blowers should operate efficiently over a range of operating conditions. For example, duct passages open and close to direct air through different heat exchangers of different flow resistances. Flow resistance typically is greatest in heater and defrost conditions, and least in air conditioning mode. In some instances, the high flow resistance of heater and defrost modes can cause performance and noise problems for conventional one-piece impellers that may be less efficient or only capable of producing relatively low pressures.
Yapp, U.S. Pat. No. 4,900,228 discloses a two-piece impeller with rearwardly curved blades with "S" shaped camber.
Chapman (WO 01/05652) discloses a two-piece impeller with high blade camber.
This invention provides blade and passage geometry found in two-piece centrifugal impellers in a design that can be injection molded as a single piece. The injection mold does not require any action or slides to mold the part.
In general, the invention features a centrifugal impeller constructed as a single part. The impeller includes three components: i) a plurality of blades, each having a leading edge and a trailing edge; ii) a generally annular top shroud connected to the tops of the blades, the top shroud having an inner radius; and iii) a hub connected to an inner portion of the base of the blades, the hub having an outer radius that is less than the inner radius of the top shroud, so that the blades, top shroud and hub can be constructed as a single unit. The invention is less expensive to manufacture than a two-piece impeller and operates more efficiently and at higher flow resistances than a conventional one piece impeller.
Another aspect of the invention is a blower assembly comprising the above described impeller and a base-plate, which, together, form an airflow path from an inlet to an outlet. The base-plate is non-rotating and extends outwardly to a radius greater than the impeller hub radius. The clearance between the base plate and the impeller blades is generally less than 10 percent of the radius of the bottoms of the blade trailing edges. In preferred embodiments, the base plate is curved in a plane which contains the impeller axis, and is contoured to match the contour of the base of the impeller blades as the impeller rotates.
In some preferred embodiments, the impeller is contained in a blower housing and said base plate is integrated into a portion of said blower housing as a single monolithic part. In some preferred embodiments, a motor is mounted to rotate the impeller, said motor being mounted to a motor flange, and said base plate is integrated into said motor flange as a single monolithic part. In some preferred embodiments, a motor is mounted to rotate the impeller, said motor being mounted in a motor housing, and said base plate is integrated into said motor housing as a single monolithic part. In some preferred embodiments, said motor housing is integrated into a portion of the blower housing as a single monolithic part.
In preferred embodiments, the blower assembly is sized and configured to be installed in an automotive climate control system.
In preferred embodiments, the impeller is characterized by:
a) a top shroud that has curvature in a plane that contains the impeller axis;
b) a cylindrical area ratio between 1.0 and 2.0;
c) an inlet to outlet area ratio between 0.7 and 1.0;
d) blades that make contact with the hub over less than 20% of the blade meanline length at the base of the blade;
e) a minimum blade chord length of 15% of the impeller diameter;
f) a blade solidity of at least 2.0;
g) tops of the blade leading edges that protrude radially inward to a radius 1-8 millimeters less than the impeller inlet radius;
h) a top shroud that covers the blades over at least 50% of the radial extent of the blades that is greater than the impeller inlet radius, and;
i) a top shroud that incorporates a ring that is used to control the recirculation through the clearance between the impeller and the blower housing.
The invention features a method of injection-molding the above-described impeller as a single piece. It also features a method of assembling a blower assembly in which a motor is attached to a motor housing, a motor flange, or a portion of a blower housing in which a base plate has been integrated, and the above-described impeller is attached to the motor in such a way as to control the clearance between the impeller and the base plate.
The details of one or more embodiments of the invention are set forth in the accompanying drawings and the description below. Other features, objects, and advantages of the invention will be apparent from the description and drawings, and from the claims.
The impeller hub 11 extends to a radius R1 that is less than the inlet radius R2, allowing one piece construction by an injection molding tool with no slides or other action.
The blade leading edges 14 extend from a radius less than the impeller hub radius R1 at the base of the blades 15, allowing the base of the blades to connect to the impeller hub 11.
The impeller top shroud 13 covers the blades and has curvature in a plane that contains the impeller axis 16. The curvature of the top shroud is designed to optimize smooth airflow through the impeller. The impeller top shroud is necessary as a structural part of the impeller. The impeller top shroud also helps to prevent flow separation and turbulence, and limits the recirculation of the flow exiting the impeller back into the blades, which results in lower operating efficiency. In preferred embodiments, the impeller top shroud can incorporate a ring 17 to provide a longer and more resistive flow path for the recirculating flow, thus reducing the amount of flow recirculating back into the impeller inlet. Additional rings can be used to further reduce the amount of recirculating flow. Also in preferred embodiments, the impeller top shroud covers over 50% of the radial extent of the blades greater than the impeller inlet radius R2.
The radius of the impeller inlet R2 and the height of the blade at that radius H2 define an inlet cylinder the area of which is 2πR2H2. The radius of the tops of the blade trailing edges R3 and the height of the blade trailing edges H3 define an outlet cylinder the area of which is 2πR3H3. The cylindrical area ratio is the ratio of the area of the inlet cylinder to that of the outlet cylinder. In the preferred embodiment, the impeller cylindrical area ratio is between 1.0 and 2.0, i.e.,
This relationship helps prevent flow separation from the top shroud surface, enabling a relatively high blower operating efficiency.
The impeller inlet area is defined as the area of a circle of radius R2. The impeller outlet area is defined as the area of a cylinder of radius R3 and height H3. The impeller inlet to outlet ratio is the ratio of these two areas. In the preferred embodiment, the impeller inlet to outlet area ratio is between 0.7 and 1.0, i.e.,
This relationship also helps prevent flow separation from the top shroud surface, enabling a relatively high blower operating efficiency.
The blade leading edge at the top of the blade protrudes radially inward to a radius less than that of the inlet. The difference between the radius of the blade leading edge at the top of the blade and the inlet radius is shown as "a". This geometry allows the half of the tool that molds the majority of the blades to extend axially to the top edge 18 of the blades 12. The two tool halves meet along this edge. In the preferred embodiment, dimension "a" is 1-8 millimeters.
Another important feature for high efficiency is high blade solidity. Blade solidity is defined as the ratio of the minimum blade chord length to the space between the blades at the furthest radial extent of the trailing edge. A blade solidity of at least 2.0 is optimal for efficient operation. Blade solidity is limited by the same phenomenon that limits blade chord length, i.e., the blade passages become so narrow as to block the airflow from progressing through the impeller, reducing operating efficiency.
A number of embodiments of the invention have been described. Nevertheless, it will be understood that various modifications may be made without departing from the spirit and scope of the invention.
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